INTEGRATED AIRBREATHING AND NON-AIRBREATHING ENGINE SYSTEM

摘要

An engine assembly includes a gas-turbine engine having a tailcone portion and a bypass duct, a rocket engine combustion assembly located at th e tailcone portion of the gas-turbine engine, and a movable nozzle segment subassembly that is selectively engageable with the gas-turbine engine bypas s duct in an open position and with the rocket engine combustion assembly in a closed position.